Non-linear spacecraft component parameters identification based on experimental results and finite element modelling-Reference-Cited by-同舟云学术

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Non-linear spacecraft component parameters identification based on experimental results and finite element modelling

Published:2016-01-11 Issue:2 Volume:8 Page:89-100
ISSN:1868-2502
Container-title:CEAS Space Journal
language:en
Short-container-title:CEAS Space J

Author:

Vismara S. O.^ORCID,Ricci S.,Bellini M.,Trittoni L.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1007/s12567-015-0110-4.pdf

Reference21 articles.

1. Allen, M.S., Sumali, H., Epp, D.S.: Restoring force surface analysis of nonlinear vibration data from micro-cantilever beams. In: Proceedings of IMECE, Chicago, Illinois (2006)

2. Crawley, E.F., O’Donnel, K.J.: Identification of non-linear system parameters in joints using the force-state mapping technique, MIT SSL report (1985)

3. Haroon, M., Adams, D.E., Luk, Y.W., Ferri, A.A.: A time and frequency domain approach for identifying nonlinear mechanical system models in the absence of an input measurement. J. Sound Vib. 283, 1137–1155 (2005)

4. Kalman, R.E.: A new approach to linear filtering and prediction problems. Trans. ASME—J. Basic Eng. 82, 35–45 (1960)

5. Kerschen, G., Soula, L., Vergniaud, J.B., Newerla, A.: Assessment of nonlinear system identification methods using the smallSat spacecraft structure, advanced aerospace applications, vol. 1, proceedings of the 29th IMAC, a conference on structural dynamics (2011)

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1. Nonlinear updating method: a review;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2017-09-09

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